What was found
DURING ROUTINE INSPECTION, THE NR 5 LEAD EDGE SLAT FOUND CRACKED AT O/B ACTUATOR ATTACH RIB. STOP DRILLED CRACK, FAB REPAIR, AND INSTALLED IAW SRM 51-40-3 & SRM 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE INSPECTION, THE NR 5 LEAD EDGE SLAT FOUND CRACKED AT O/B ACTUATOR ATTACH RIB. STOP DRILLED CRACK, FAB REPAIR, AND INSTALLED IAW SRM 51-40-3 & SRM 51-30-2.